Criteria

Text:
Sector:
Content:
Display:

Results

Viewing 1 to 30 of 4998
2014-10-31
WIP Standard
ARP6316
This SAE Aerospace Recommended Practice (ARP) documents a common understanding of terms, compliance issues and occupant injury criteria to facilitate certification of oblique facing seat installations specific to Part 25 aircraft.
2014-10-30
Standard
AIR5026B
This document discusses, in broad general terms, typical present instrumentation practice for post-overhaul gas turbine engine testing. Production engine testing and engine development work are outside the scope of this document as they will typically use many more channels of instrumentation, and in most cases will have requirements for measurements that are never made in post-overhaul testing, such as fan airflow measurements, or strain measurements on compressor blades. The specifications for each parameter to be measured, in terms of measurement range and measurement accuracy, are established by the engine manufacturers. Each test cell instrument system should meet or exceed those requirements. Furthermore, each instrument system should be recalibrated regularly, to ensure that it is still performing correctly.
2014-10-30
Standard
ARP5794
This specification covers the general requirements for aircraft tank mounted, centrifugal type, fuel booster pumps, used for engine fuel feed and/or fuel transfer.
2014-10-22
WIP Standard
AIR1351J

This SAE Aerospace Information Report (AIR) covers the general requirements for and the listing of manufacturers identification that appear on electrical/electronic wiring devices and accessories as required by individual product specifications. Supplier markings from previous submitted listings are maintained for component traceability.

2014-10-22
WIP Standard
GEIASTD0009A
This standard requires the developers and customer/user's working as a team to plan and implement a reliability program that provides systems/products that satisfy the user's requirements and expectations. The user's requirements and needs are expressed in the form of the following four reliability objectives: The developer shall solicit, investigate, analyze, understand and agree to the user's requirements and product needs. The developer, working with the customer and user, shall include the activities necessary to ensure that the user's requirements and product needs are fully understood and defined, so that a comprehensive design specification and Reliability Program Plan can be generated; The developer shall use well-defined reliability- and systems-engineering processes to develop, design, and verify that the system/product meets the user's documented reliability requirements and needs. The developer shall implement a set of engineering activities (included in this standard as normative activities and informative activities, refer to Section 3) so that the resulting system/product satisfies the customer's documented requirements and needs; The multifunctional team shall verify during production that the developer has met the user's reliability requirements and needs prior to fielding.
2014-10-22
WIP Standard
ARP4741A
This SAE Aerospace Recommended Practice (ARP) establishes the requirements for the design, manufacture, and qualification of four hydraulic switching valves used in airborne applications. Two are pressure operated, Type IA and IB and two are solenoid/pilot operated, Type IIA and IIB. They are applicable to four pressure classes 3000, 4000, 5000 and 8000 psi. The equipment as designed is intended to be installed in hydraulic systems designed to AS5440 for military applications or ARP4752 and ARP4925 depending on the type of aircraft for commercial applications. Additional or refined requirements shall be contained in the detail (procurement) specification and these shall take precedence over any potentially conflicting requirements of this ARP or documents referenced by this ARP.
2014-10-22
WIP Standard
AS7997A
This specification covers constant displacement hydraulic motors, generally remotely mounted, using hydraulic fluid under pressure as the energy transfer medium for driving various accessories. Hydraulic motors shall be suitable for use in aircraft hydraulic systems conforming to and as defined in MIL-H-5440 and MIL-H-8891 as applicable.
2014-10-20
WIP Standard
ARP1821B
This SAE Aerospace Recommended Practice (ARP) includes recommendedground flotation analysis methods for both paved and unpaved airfields. The purpose of this document is to identify the recommended aircraft ground flotation analysis methods that should be used for aircraft landing gear design.
2014-10-16
WIP Standard
AMS2630D
This specification covers procedures for ultrasonic inspection, by pulse-echo procedures, of flat, rectangular, round, cylindrical, and contoured products having a thickness or cross-sectional dimension greater than 0.50 inch (12.7 mm), using either contact or immersion methods, and using the longitudinal-wave or shear-wave modes or combinations of the two, as necessary. This specification may apply to testing finished machined parts provided the parts can meet the basic testability requirements, such as size, contour, metallurgical structure, and thickness.
2014-10-08
Standard
ARP6200
This SAE Aerospace Recommended Practice (ARP) describes the recommended tests and their associated test means for commercial aircraft hydraulic systems at the system level that are required to demonstrate compliance with the 14 CFR Part 25 and EASA CS 25 airworthiness regulations, and to show that the required level of maturity at the aircraft entry into service (EIS) has been achieved.
2014-10-08
Standard
AS5127/1C
This SAE Aerospace Standard (AS) describes test methods to determine the application and performance properties of two-component sealing compounds. It shall be used in conjunction with AS5127 and the applicable material specification. When modifications to these test methods are called out in material specifications, the material specification shall take precedence.
2014-10-06
Standard
AS9102B
This standard establishes the baseline requirements for performing and documenting FAI. Should there be a conflict between the requirements of this standard and applicable statutory or regulatory requirements, the applicable statutory or regulatory requirements shall take precedence.
2014-10-02
WIP Standard
AS23053/1
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/11
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/10
This detail specification establishes the requirements for a type of electrical insulating sleeving that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/12
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/13
This detail specification establishes the requirements for a type of electrical insulating sleeving that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/15
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/18
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/14
This detail specification establishes the requirements for a type of electrical insulating sleeving that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/16
This detail specification establishes the requirements for a type of electrical insulating sleeving that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/8
This detail specification establishes the requirements for a type of electrical insulating sleeving that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/6
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/7
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/4
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-10-02
WIP Standard
AS23053/5
This detail specification establishes the requirements for a range of similar electrical insulating sleevings that will shrink to a predetermined size upon the application of heat.
2014-09-30
WIP Standard
AS81936/3
This SAE Aerospace Standard will cover airframe plain spherical bearings ustilizing a Copper Nickel Tin ball and a Corrosion Resistant Steel outer race for use between -65F and+350F.
2014-09-30
WIP Standard
AS81936/4
This SAE Aerospace Standard will cover airframe plain spherical bearings ustilizing a Copper Nickel Tin ball and a Corrosion Resistant Steel outer race for use between -65F and+350F.
2014-09-30
WIP Standard
AS17108B
The intent is to ballot this drawing package and then stabilize it.
Viewing 1 to 30 of 4998

Filter

  • Aerospace
    4998
  • Standard
    4998